Polyimide composition and method for protecting photoreactive cells

ABSTRACT

A protective coating for solar cells, particularly solar cells positioned in space and which coating is a polyimide which is colorless, transparent, relatively non-brittle, has a high degree of thermal stability and readily transmits solar radiation without appreciable degradation. The coating is heat resistant and does not degrade significantly when exposed to ultraviolet radiation, and is highly effective in repelling low energy proton particles. In a preferred embodiment, the protective polyimide coating is a polymer having the following recurring structural unit: ##STR1##

This is a division of application Ser. No. 451,137, filed Dec. 20, 1982,now abandoned.

BACKGROUND OF THE INVENTION

1. Field of the Invention

This invention relates to a polymeric coating for solar cells and to apolymer coated solar cell, and is particularly directed to polyimidecoatings for solar cells and solar cells coated with such polyimides andwhich coatings are colorless and transparent, relatively non-brittle,have good thermal properties, resistance to ultraviolet radiationdegradation, effective in repelling low energy protons and also haveother desirable characteristics for use in outer space.

2. Description of the Prior Art

Polymeric coatings for solar cells are required to provide a high degreeof solar radiation protection. Conventional polyimides have therequisite thermal stability, but they are colored, and thus absorb inthe visible portion of the solar spectrum which reduces performance andgenerates heat which promotes degradation. Other polymers discolorexcessively or lose structural integrity for various other reasons, suchas instability to solar protons, electrons, or ultraviolet radiation.When these polymer coatings discolor, the portion of solar spectrumtransmitted to the solar cells is reduced, thus effectively reducing thesolar cell efficiency.

In the prior art, coatings such as polyurethanes, epoxies, polyesters,polyimides, etc., were evaluated and found to have inadequate stabilityfor various reasons. Perfluorinated aliphatic hydrocarbons, such as FEPTeflon (tetrafluoroethylene hexafluoropropylene copolymer), had a betterpotential, but had inadequate stability. Further, it is necesssry toemploy an adhesive or a fusion process in order to apply the Teflon orother polymer coating to the solar cell itself. Usually such an adhesiveis a silicone. However, after a period of time, the adhesive or fusionboundary fails and the Teflon becomes separated from the solar cell,thereby accelerating deterioration and failure of the cell.

Because of the limitations of known polymers heretofore used orconsidered for solar cells, and particularly for solar cells positionedin outer space, it was necessary to employ a quartz cover over the solarcell itself, in order to protect the cell against low energy particlessuch as low energy proton bombardment. However, the quartz layer wasusually quite heavy (relative to a polymeric coating). This quartz layerthus increased the overall weight and made introduction of the solarcell into very large arrays much more difficult and costly.

Some of the commonly used protective covers for solar cells are formedof fused silica. These fused silica layers usually require a multi-layerfilter to effectively filter out all ultraviolet radiation, as forexample, that radiation less than 0.35 μm, to protect the adhesive(e.g., a silicone adhesive) from darkening and losing transmission andhence power. Another protective cover commonly used is Ceria, namely acerium oxide doped glass micro-sheet. This glass sheet has a naturalcut-on frequency of about 0.35 μm and hence does not require amulti-layer filter for adhesive protection. The Ceria glass sheet doesprovide for radiation stability.

In addition to the foregoing, a fused silica without a multi-layerfilter has been used with the FEP Teflon as the adhesive. Thiscombination is quite effective in view of the fact that glass processingis minimized. However, the overall covered solar cell is still too heavyfor use as a space cell in extremely large solar cell arrays.

The method of protecting solar cells which is currently used to a largedegree involves the adhesive bonding of a thin ZnO/Ta₂ O₅ coated quartzcoverslide onto the solar cells with a silicone adhesive. Themulti-layer ZnO/Ta₂ O₅ coating on the quartz is a solar radiationcut-off coating which provides damaging solar radiation (approximatelyless than 0.32 μm) from penetrating through the quartz into the siliconeadhesive. Although this means of protecting solar cells is effective, itis too expensive and impractical to apply to massive solar arrays, suchas those which would be required for capturing solar radiation on amassive scale in space and transmitting it to earth. This technique ispractical only for relatively "small" devices such as communicationsatellites where the added costs can be tolerated. It is not practicalfor large size applications, e.g., acre size applications.

Consequently, there still exists a need for a much more reliable, lightweight, protective coating for solar cells, and particularly for thosesolar cells which are to be exposed to outer space environments. Theprior art cover materials or coating materials such as quartz and theother polymers, are of limited effectiveness. The polymer systems,particularly, suffer from the disadvantge in that they exhibit loss oftransmission, cracking and loss of adhesion to the cell after exposureto solar ultraviolet radiation for any reasonable period of time.Further, adhesion is affected materially after subjection to the outerspace environments. Consequently, the critical properties for solar cellcoatings include the property of being resistant to ultravioletradiation and maintaining optical clarity, even after a period of time.These coatings must also be resistant to degradation by low energyprotons and exhibit good adhesion to the cell after some thermalcycling. Further, they must be formulated for ease of application to thesolar cells without any damage to the cell itself. In addition, thecoatings must be formulated to be more cost effective than thepreviously and presently used quartz and glass systems.

U.S. Pat. No. 3,356,648 discloses linear polyimides derived from thehexafluoroisopropylidene bridged diamine, such as dianiline, andtetracarboxylic dianhydride. These polyimides are useful as shapedstructures and for wrappings, packaging and the like.

U.S. Pat. No. 3,959,350 discloses linear polyimides similar to those ofU.S. Pat. No. 3,356,648, but which do not have hexafluoroisopropylidenegroups bridging the amine moieties. These polyimides are useful asmolding compounds, and for preparing self-supporting film structures andcomposites. However, these polyimides are not colorless. The lack oftransparency and the other physical characteristics, such asprocessability of these ppolyimides, render them ineffective as solarcell coatings.

SUMMARY OF THE INVENTION

According to the invention, solar cells are coated with a polymer in theform of a polyimide to form a protective coating thereon. The coating isa polyimide which has the following specific properties. The polyimide(1) is colorless, (2) is transparent to the solar radiation in thevisible light spectrum, (3) is relatively non-brittle, (4) has a highdegree of thermal stability, (5) readily transmits solar radiationwithout appreciable degradation, (6) is heat resistant, (7) does notdegrade significantly when exposed to ultraviolet radiation, and (8) ishighly effective in protecting against low energy particles, such asproton particles, by effectively absorbing such particles.

In a more preferred embodiment, the coating is formed from a polyimidecomposition which has the recurring structural unit shown below:##STR2## where R is: ##STR3## and n has a value range from 10 to about2000. Preferably, n has a value from about 10 to about 1000.

The polyimide which is most preferred according to the invention is themeta amino phenylene derivative of formula II above, and having therecurring structural unit: ##STR4## and its precursor has the polyamicacid structure: ##STR5## where n has the values noted above.

It has been found that the above polyimide, particularly of structure IVabove, when applied as a coating to a solar cell has excellentresistance to degradation from solar radiation and particularlyradiation in the ultraviolet wave length range. The film also hasremarkable proton absorption capabilities. It has been noted that noother polymer coatings evaluated to date provide the degree of solarradiation protection afforded by the polyimide coatings of the structureof formula I above, and especially of formula IV while providing theadvantage of these coatings.

More particularly, the above polyimide coating is highly suitable forsolar cell coating application because of its unique combination ofproperties. This unique combination of properties includes theirexcellent thermal stability, which is at least equivalent to that ofother aromatic polyimides, transparency in films, colorless nature,stability to ultraviolet radiation, and ability to protect against lowenergy proton and electron bombardment. This combination of propertiesis essential for a coating to be useful in the protecting of solarcells.

A particular advantage of the solar cell coatings of this invention istheir capability for use without the quartz cover heretofore employed onsolar cells and without the need for an adhesive layer susceptible toultraviolet light degradation.

This invention possesses many other advantages and has other purposeswhich may be made more clearly apparent from a consideration of theforms and compositions in which it may be embodied. They will now bedescribed in detail for the purposes of more fully setting forth thegeneral principles of the invention, but it is to be understood thatsuch detailed description is not to be taken in a limiting sense.

BRIEF DESCRIPTION OF THE DRAWING

In the accompanying drawing, the FIGURE is a vertical section view of asolar cell having a coating in accordance with the present inventionapplied thereto.

DETAILED DESCRIPTION OF THE INVENTION

Referring now in more detail and by reference characters to the drawing,there is shown a solar cell having a polyimide coating as hereinafterdescribed. The photocell itself generally comprises a base of p-typesemiconductor material which constitutes a p-layer 10 and which is dopedon one surface with an n-type material forming an n-layer 12 having ap-n junction 14 therebetween.

A p-layer electrode 16 is attached to the bottom side of the p-layer 10for an electrical conductor to be connected thereto. An n-layerelectrode 18 may be connected to the n-layer 12 to enable an electricalconductor to be connected thereto. The n-layer electrode usuallyincludes a number of so-called relatively thin fingers extendingthroughout the surface area of the n-layer so as to avoid anysubstantial interference with visual light radiation impingement on thephotocell.

The photoreactive layers or so-called "photo-voltaic" layers includingthe n-layer 12 and p-layer 10 and junction 14 may adopt the form of asilicon material or it may be a III-V compound such as gallium arsenide,gallium arsenide-phosphide, etc. Other photo-voltaic materials wellknown in the art may be employed and may be properly doped.

In maby cases, an anti-reflective coating 20 may be employed and wouldbe deposited directly on the active surface of the cell prior toapplication of the polyimide protective coating. A suitableanti-reflective coating is a combination of TiO_(x) and Al₂ O₃, Ta₂ O₅or SiO_(x).

Prior to the application of a polyimide coating 22 prepared inaccordance with the present invention, a primer coating 24 may beapplied to the upper surface of the n-layer 12 or to the anti-reflectivecoating 20, if employed. The primer coating 24 would generally increasethe adhesion of the polyimide coating to the solar cell and particularlyto the upper surface of the anti-reflective layer 20 thereof. A typicalprimer for this purpose is a silane adhesion promoter, such asaminopropyltrimethoxysilane. Other silane adhesion promoters are alsoknown in the art and might also be used for this purpose.

The polyimide of formula IV above is prepared by the reaction ofsubstantially equal molar proportions of the two monomers2,2-bis(3-aminophenyl)hexafluoropropane and4,4'-hexafluoroisopropylidene[bis(phthalic anhydride)], in a solvent forsuch monomers. The solvents which can be used include, for example,tetrahydrofuran, N-methyl pyrrolidinone, N-methylformamide,dimethylformamide and N,N-dimethylacetamide and mixtures thereof. Theresulting polyamic acid solution can be cast as a film and the filmimidized to the polyimide structure IV above. Both the polyamic acid andthe polyimide have an inherent viscosity of at least 0.1, usually0.3-0.5. The inherent viscosity of the polyimide is measured at 30° C.as a 0.5% solution in a suitable solvent, such as cold concentrated(96%) sulfuric acid, or methanesulfonic acid.

As noted above, in preparing the coated solar cells according to theinvention, a solution of the polyamic acid precursor of formula V abovein a solvent, such as tetrahydrofuran, at a concentration of about 10 toabout 30% of the polyamic acid, can be used as a varnish for applicationto the active surface of a solar cell.

The varnish or solution of the polyamic acid precursor can be coatedover the primer coating 24 of the solar cell in any suitable manner, forexample, by dipping, electrocoating, spraying, electrostatic sprayingand the like. Spraying is a convenient method of application, ascontrasted, for example, to the use of Teflon applied as a solar coatingaccording to the prior art, and which requires application of a film. A15% solids content solution of the polymer in N-methylpyrrolidinone ordimethylformamide has been found to be effective. The solution issprayed after applying the primer (A1100, aminopropyltrimethoxysilane)from a 5% solution in ethanol. The amount of the polyamic acid in thesolvent will vary depending primarily on the type of sprayer or othercoating means which is used. The solid content of the polyamic acid inthe solvent solution can vary greatly and could be as high as 30% intetrahydrofuran and in which solution dimethylformamide can be present,in an amount of normally at least 60%.

After application of the polyamic acid varnish to the solar cell, thatis, over the primer, the solvent is essentially evaporated off and theamic acid polymer is converted into the imidized or polyimide structureof formula IV by heating such amic acid polymer at about 250° C. Lowertemperatures, such as at 120° C., can also be used to promote theimidization, but the reaction rate is slower and the elimination ofsolvent residues is slower. Preferred imidization temperatures rangebetween about 160° C. and 250° C. The polyimide coating may also bedried at 350° F. (about 175° C.) in a vacuum bag. Thinner coatings(about 0.1 mil thick) can be dried and then cured for 1 to 2 hr. at 485°F. (about 250° C.) in a vacuum bag. However, the preferred temperaturefor effecting imidization is that which provides the best solar cellperformance, and this may vary depending upon the specific type of celland the specific batch of amic acid polymer available.

The polyimide film 22 thus formed is generally a very thin layer, as isthe silane primer film. The polyimide film itself is preferably about0.2 to 0.5 mil thick. However, the practical minimum thickness is about0.1 mil. There is no absolute maximum thickness, except that the filmshould be as thin as possible and yet provide the desiredcharacteristics to minimize weight of the solar cell.

EXAMPLES

The invention is further illustrated by, but not limited to, thefollowing examples:

EXAMPLE I

This example I discloses the preparatition of the polyimide and itscasting into a film.

A 100 ml three-necked flask was fitted with a stirrer and gas inlet andoutlet tubes. The flask was charged with a solution of2,2-bis(3aminophenyl)hexafluoropropane. (1.6344 grams, 0.004890 mole) in30 ml of purified N,N-dimethylacetamide. Under an argon atmosphere atroom temperature and with good stirring, powdered solid4,4'-hexafluoroisopropylidenebis(phthalic anhydride) (2.1700 grams,0.004890 mole) was added over a three minute period. The solution wasstirred overnight under argon. The solution increased in viscosityduring this time. A clear colorless film could be cast from the solutionand after drying at 75° C. in an air circulating oven, the film could beimidized by heating above 200° C. to form a clear and colorless filmafter imidization.

EXAMPLE II

A solution of varnish of about 15% of the polyamic acid precursor offormula V above in 25% tetrahydrofuran, and containing about 60% ofdimethylformamide was prepared in a manner as essentially disclosed inExample I above. The varnish was applied by spraying over the silicacovers of a K63/4 solar cell, where K63/4 designates a shallow diffused10 ohm-cm silicon solar cell with a back surface field and reflector.

After application of the amic acid coating to the solar cell, thecoating was heated at about 250° C. for a period of about 60 minutes,causing substantially all of the solvent to evaporate off, andconverting the polyamic acid to a colorless transparent film of thepolyimide of structure IV above. A 0.5 mil thick colorless transparentpolyimide coating was thus formed on the solar cell.

In a 1200 hour test of the 0.5 mil polyimide coating of the typespecified above, under a Xenon light source equivalent to 1.5 suns of UVexposure, the net loss in short circuit (I_(sc)) corresponding to UVtransmittance loss, showed an estimated net UV loss (I_(sc)) of only8.1%, and with a 0.2 mil polyimide coating, ws only 8.4%. This loss wasan order of magnitude less than that which has been observed with otherpolymeric coatings such as polyurethanes, epoxies or polyesters,indicating only very minor degradation of the polyimide coating due toUV exposure as compared to other polymeric coatings.

EXAMPLE III

Thermal cycling of the polyimide coated solar cells (0.2 and 0.5 milcoating) for Example II (room temperature to liquid nitrogen, 25 cycles)showed no loss of adhesion, via a tape pull test, of the coating to thecell substrate. The tape pull test involves the application of anadhesive tape, such as a Scotch Brand number 600 tape or the equivalent,to the solar cell and particularly the n-layer electrode and the p-layerelectrode surfaces. The tape is pulled away from these contacts orelectrodes with a continuous pull. The pull is initiated at one end andprogresses toward the other. The cell is then examined for conformanceto a desired adhesion level.

Exposure of the coated cells (0.2 mil and 0.5 mil coating) to simulatedspace radiation showed essentially no loss in short circuit current.Dosages of 1×10¹¹ protons/cm² (50 KeV) and 2×10¹¹ protons/cm² (50 KeV)gave identical results. Spectral response was measured before and afterproton exposure. No significant changes were noted, thus indicatingresistance of the polyimide solar cell coatings to proton radiation.

Several additional tests were conducted with the standard 10 ohm-cmshallow diffused silicon solar cells designated as the K6 solar cells.These cells had a back surface field and a back surface reflector. Insome cases, tests were conducted with solar cells having a texturedfront surface designated as the K-7 cells. Tests were generallyconducted with thicknesses of the polyimide films of about 0.2 and 0.5mil. Further, the thickness variation of the polyimide layer did notapparently have any significant influence on the amount of ultravioletdegradation. Consequently, relatively thin films can be employed.

From the foregoing, it is seen that the invention provides an improvedpolymer coated solar cell with a specific polyimide coating having thefollowing advantages: a colorless polymeric coating is provided whichreadily transmits solar energy, does not degrade significantly whenexposed to proton radiation, electron radiation and ultraviolet light;is transparent and heat resistant, and protects the solar cell from thedamaging effects of solar protons, electrons, ultraviolet light andother forms of radiation, is a relatively non-brittle film formingcoating, and has processing characteristics which permit it to bereadily coated onto solar cells.

The specific polyimide coatings of the present invention obviate theproblems heretofore described. These coatings are very light in weightdue to the fact that they can be applied in very thin coatings andnevertheless still provide the necessary protection. For example, a 0.2mil coating has been found to be highly effective. Further, the lowmolecular weight of the polymers may provide for good adhesion to thesolar cell itself. In addition, this also enables the adhesion to bemaintained over a long lifetime. Indeed, exposure of the solar cellscoated with the polyimide resin of the invention with a thickness of 0.2mil to 0.5 mil and subjected to simulated space radiation showedessentially no loss in short circuit current. Spectral response was alsomeasured before and after exposure to low energy protons. Once again, nosignificant changes were noted and the polyimide coated solar cellpermitted effective transmission of solar radiation in the range of 0.32μm to 0.96 μm.

Thus, there has been described a novel polyimide composition and methodfor protecting photoreactive cells, such as solar cells, and whichcomposition and method provides a coating which is relatively durable,tightly adherent and capable of withstanding ultraviolet radiationdegradation and bombardment by low energy particles. This compositionand method thereby fulfills all of the objects and advantages soughttherefor. It should be understood that many changes, modifications,variations and other uses and applications will become apparent to thoseskilled in the art after considering this specification and theaccompanying drawing. Therefore, any and all such changes,modifications, variations and other uses and applications which becomeapparent to those skilled in the art after considering thisspecification are deemed to be covered by the invention which is limitedonly by the following claims.

What is claimed is:
 1. A method for applying a substantially colorlesstransparent protective heat resistant polymeric coating to a solar cell,said coating transmitting radiation and having high resistance to lowenergy protons, electron bombardment and resistance to ultraviolet lightdegradation, which comprises:(a) applying a solution of polyamic acid toa solar radiation transmitting component of a solar cell, said polyamicacid having the recurring structural unit: ##STR6## and (b) heating saidpolyamic acid to convert same to the polyimide in the form of a filmhaving the recurring structural unit: ##STR7## and where n is a numberranging from 10 to about
 2000. 2. The method as defined in claim 1, saidpolyamic acid being formed by reacting equal molar proportions of thetwo monomers 2,2-bis(3-aminophenyl)hexafluoropropane and4,4'-hexafluoroisopropylidenebis(phthalic anhydride), in a solvent forsuch monomers.
 3. The method as defined in claim 2, said solutioncontaining a solvent selected from the group consisting oftetrahydrofuran, N-methyl pyrrolidinone, N-methylformamide,dimethylformamide and N,N-dimethylacetamide, and mixtures thereof.
 4. Animproved method of protecting the photoreactive portion of a photocellby applying a protective coating to said reactive portion, theimprovement comprising applying to said photoreactive portion a coatingwhich is substantially colorless and transparent, heat resistant andhaving high degradation resistance to radiation in the ultravioletspectrum and resistance to low energy particles, and which coatingcomprises a polyimide having the recurring structural unit: ##STR8##where R is: ##STR9## and where n is a number ranging from 10 to about2000.